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发明公开
CN106837430A 带有膜孔的燃气涡轮发动机 无效 - 驳回

带有膜孔的燃气涡轮发动机
摘要：
本发明涉及带有膜孔的燃气涡轮发动机。具体而言，一种用于燃气涡轮发动机(10)的发动机构件(120)可产生热燃烧气流(H)且提供冷却流体流(C)。壁(122)可将热燃烧气流(H)与冷却流体流(C)分开。多个膜孔(130)可布置在壁(122)中，膜孔具有邻近冷却流体流(C)的入口(132)和在热燃烧气流(H)处的出口(134)，使得可提供冷却流体流(C)至热燃烧气流(H)。膜孔(130)还包括入口(132)，使得入口(132)可配置有相对于彼此具有至少一个不同定向或彼此不对准的入口(132)。
摘要（英）：

The invention relates to a gas turbine engine with film holes. Concretely, An engine component (120) for a gas turbine engine (10) can generate a hot combustion gas flow (H) and provide a cooling fluid flow (C). A wall (122) can separate the hot combustion gas flow (H) from the cooling fluid flow (C). Multiple film holes (130) can be disposed in the wall (122), having an inlet (132) adjacent the cooling fluid flow (C) and an outlet (134) at the hot combustion gas flow (H) such that the cooling fluid flow (C) can be provided to the hot combustion gas flow (H). The film holes (130) further comprise inlets (132), such that the inlets (132) can be arranged with the inlets (132) having at least one of a different orientation relative to one another or are non-aligned with each other.

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